View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 40012U 14033C 24357.87251228 .00006233 00000-0 75596-3 0 9993
2 40012 97.7193 153.2414 0050646 49.4538 311.1069 14.83000507565778
Epoch (UTC): | 22 December 2024 20:56:25 |
Eccentricity: | 0.0050646 |
inclination: | 97.7193° |
perigee height: | 584 km |
apogee height: | 655 km |
right ascension of ascending node: | 153.2414° |
argument of perigee: | 49.4538° |
revolutions per day: | 14.83000507 |
mean anomaly at epoch: | 311.1069° |
orbit number at epoch: | 56577 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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